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M-V

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Mu-5 M-5

M-V
1:110 Scale
H:28.0 cmD:2.3 cm
~29 bricks tall~3 studs wide
Maiden Launch1997-02-12
Family: Mu
Designer: ISAS·Manufacturer: MHI·Operator: JAXA·Commissioner: ISAS
3–4 Stages
Height / Length
30.8 m
Diameter
2.5 m
Launch Mass
139,000 kg
Takeoff Thrust
3,792 kN
LEO Capacity
1,850 kg

Mission Profile

The M-V (Mu-5, M-5) was a three-to-four-stage Japanese solid-fuelled launch vehicle in the Mu family, the largest and most powerful all-solid rocket ever operated, developed by ISAS for scientific satellite delivery. Standing 30.8 m tall with a 2.5 m core diameter and a liftoff mass of 139 tonnes, it generated 3,792 kN of first-stage thrust and could deliver 1,850 kg to low Earth orbit. First flying in February 1997, the M-V launched the HALCA radio astronomy satellite, Hayabusa asteroid sample return mission, and several other important Japanese scientific missions before being retired in 2006.

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